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The Apollo Spacecraft - A Chronology [Vol 3] by National Aeronautics and Space Administration

By National Aeronautics and Space Administration

This 3rd quantity of the Apollo Spacecraft Chronology covers the sixteen-month interval from October 1, 1964, to January 20, 1966. in this interval the key emphasis of this system was once at the particular engineering of the 3 spacecraft being synthetic by means of North American and Grumman. All significant judgements were made and now in the confines of those judgements spacecraft needs to be designed and equipped that may adequately offer transportation for males and kit to the lunar floor and again. probably the most confining of those judgements was once the agreed upon payload of the Saturn V. It used to be firstly agreed that the layout allowable weight for the Apollo spacecraft used to be ninety 000 kilos. incorporated inside of this have been the Command and repair Module, the Lunar expedition Module, and the adapter constitution. even if a few reduction used to be received whilst the conservatism within the Saturn V layout used to be switched over into extra priceless functionality, spacecraft weight used to be a continuing obstacle within the Apollo application. This was once relatively precise in the course of the interval pronounced upon during this quantity; techniques have been being translated into difficult layout and the answer of diverse information took their toll in an upward revision of weight estimates. Weights have been pronounced weekly in an try and curtail and regulate weight development. courses have been instituted to lessen weight through the removing of nonessential "niceties" and, whilst functional, through remodeling parts to lighter weight.

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25 ASPO Manager C. Phillips tractors that (Space Joseph F. Shea it was his desire Technology final evaluation and Shea had MSC's accomplish asked C. H. Lambert, Belew, MSFC; Lewis Research W. the Maxime and F. Rector C. and A. Faget would also III, H. Rocketdyne) for the 32 to R. to to serve: all of MSC; _V. the engine. of a committee Grumman; Maj. Samuel subcon- descent individuals J. G. Thibodaux, OMSF; two prior LEM following J. A. Gavin, King, Director of the to be chairman ask the and and Program progress of a subcontractor M.

Of the by July MSC, to Chief, 16, 196,1. orbit the proposals the deliveries the earth in that the 1, 1965: Johnston, No_ember use CHRONOLOGY Manager projected 15, 1965; simulator A for to the It was by June two qualified l,ettcr, Richard S. labotic simulator," 16-December assigned by January awarded SPACECRAFT: t)e compatible t)een System be completed contract APOLLO the just once, (at MAT mated simulated to T and minus removed the flights launch and ADVANCED would be evaluated. DESIGN, reconnected only FABRICATION, after data AND from TESTING the had simulation been 1964 November .

Rules to determine garment 19-26 of the C. 5 and life support the 19-26 system and doffed and with kilonewtons of redesigning the of excess material for doffing donned condition 19-26 defined. protection in donning and pressurized total unit weight for the reliability design mobility per sq m ETG in the neck which restricted visibility. MSC, "ASI'O Francis 9-2820," Weekly J. DeVos, November Officials from container North would movable hard MSC, "ASPO MSC, to To ensure consistent that with packed Attn: November Systems and stowage stowage Weekly disposition," Crew American container NAA, Report, Chief, and be spacecraft's change Management MSC, to 19, 1964.

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